View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57399U 26145.59699876 +.00000000 +00000-0 +20694-3 0 00007
2 57399 97.2609 196.7875 0002302 172.1658 187.9620 15.29501036 03
| Epoch (UTC): | 25 May 2026 14:19:40 |
| Eccentricity: | 0.0002302 |
| inclination: | 97.2609° |
| perigee height: | 476 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 196.7875° |
| argument of perigee: | 172.1658° |
| revolutions per day: | 15.29501036 |
| mean anomaly at epoch: | 187.9620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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